RU2002114395A - Gas turbine unit - Google Patents

Gas turbine unit

Info

Publication number
RU2002114395A
RU2002114395A RU2002114395/06A RU2002114395A RU2002114395A RU 2002114395 A RU2002114395 A RU 2002114395A RU 2002114395/06 A RU2002114395/06 A RU 2002114395/06A RU 2002114395 A RU2002114395 A RU 2002114395A RU 2002114395 A RU2002114395 A RU 2002114395A
Authority
RU
Russia
Prior art keywords
gas turbine
turbine unit
duct
outlet
bypass
Prior art date
Application number
RU2002114395/06A
Other languages
Russian (ru)
Other versions
RU2224901C1 (en
Inventor
Александр Юрьевич Степанов (RU)
Александр Юрьевич Степанов
Юрий Михайлович Ануров (RU)
Юрий Михайлович Ануров
Борис Владимирович Сударев (RU)
Борис Владимирович Сударев
Александр Борисович Тараканов (RU)
Александр Борисович Тараканов
Владимир Михайлович Ширманов (RU)
Владимир Михайлович Ширманов
Original Assignee
Энергомаш (Юк) Лимитед (Gb)
Энергомаш (Юк) Лимитед
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Энергомаш (Юк) Лимитед (Gb), Энергомаш (Юк) Лимитед filed Critical Энергомаш (Юк) Лимитед (Gb)
Priority to RU2002114395/06A priority Critical patent/RU2224901C1/en
Publication of RU2002114395A publication Critical patent/RU2002114395A/en
Application granted granted Critical
Publication of RU2224901C1 publication Critical patent/RU2224901C1/en

Links

Claims (1)

Газотурбинная установка с регулированием тепловой мощности, содержащая газотурбинный блок, включающий компрессор, камеру сгорания и турбину, установленный последовательно с ним по газу регенератор, сообщенный подводящим воздуховодом с выходом компрессора, а отводящим воздуховодом с камерой сгорания и утилизационный теплообменник, отличающаяся тем, что она снабжена соединяющим подводящий и отводящий воздуховоды байпасным воздуховодом и устройством для регулирования расхода воздуха, проходящего по отводящему и байпасному воздуховодам, которое выполнено или в виде трехходового клапана, установленного в месте соединения байпасного и отводящего воздуховодов, или в виде установленных в байпасном и отводящем воздуховодах отдельных регулирующих клапанов.A gas turbine unit with thermal power control, comprising a gas turbine unit including a compressor, a combustion chamber and a turbine, a regenerator installed in series with it through a gas, connected by a supply duct to the compressor outlet, and a discharge duct with a combustion chamber and a recovery heat exchanger, characterized in that it is provided connecting the supply and exhaust ducts with a bypass duct and a device for controlling the flow rate of air passing through the exhaust and bypass ducts um, which is formed or as a three-way valve installed at the junction of the bypass duct and outlet, as mounted in the bypass duct and outlet of separate control valves.
RU2002114395/06A 2002-05-31 2002-05-31 Gas-turbine plant RU2224901C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2002114395/06A RU2224901C1 (en) 2002-05-31 2002-05-31 Gas-turbine plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2002114395/06A RU2224901C1 (en) 2002-05-31 2002-05-31 Gas-turbine plant

Publications (2)

Publication Number Publication Date
RU2002114395A true RU2002114395A (en) 2004-01-10
RU2224901C1 RU2224901C1 (en) 2004-02-27

Family

ID=32172766

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2002114395/06A RU2224901C1 (en) 2002-05-31 2002-05-31 Gas-turbine plant

Country Status (1)

Country Link
RU (1) RU2224901C1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9028206B2 (en) * 2012-06-12 2015-05-12 General Electric Company Thermally actuated assembly for a gas turbine system and method of controlling a cooling airflow path
RU2628851C1 (en) * 2016-10-25 2017-08-22 федеральное государственное бюджетное образовательное учреждение высшего образования "Национальный исследовательский университет "МЭИ" (ФГБОУ ВО "НИУ "МЭИ") Gas turbine plant

Also Published As

Publication number Publication date
RU2224901C1 (en) 2004-02-27

Similar Documents

Publication Publication Date Title
WO2006052797A3 (en) Exhaust system and method for controlling exhaust gas flow and temperature through regenerable exhaust gas treatment devices
JP2008002466A (en) Air bypass system and method for gas turbine inlet
FR2847005A1 (en) Improved regulation of air intake temperature and recirculated exhaust gas temperature, uses control of entry of exhaust gas and a controlled bypass to control heat exchange between exhaust gas, intermediate fluid and intake air
FR2847004A1 (en) Temperature regulation for engine intake air and recirculated exhaust gas, uses single unit housing two heat exchangers to exchange heat between exhaust gas, fluid and intake air, with control of fluid flow
RU2002123226A (en) GAS HEAT PUMP TYPE AIR CONDITIONING DEVICE
RU2008135292A (en) VENTILATION AND INFLATING TURBO MACHINE COMPONENTS
GB2394038B (en) Recuperative exhaust-gas heat exchanger for a gas turbine engine
RU2002114395A (en) Gas turbine unit
ZA202306737B (en) Air supply mechanism for biomass hot-blast stove
RU2005107887A (en) ENERGY INSTALLATION
RU2004103042A (en) GAS-TURBINE ENGINE TURBINE COOLING SYSTEM
RU2007142364A (en) GAS-TURBINE POWER INSTALLATION
RU2440502C1 (en) Air-cleaning device for gas-turbine plant
RU174364U1 (en) GAS-PUMPING UNIT WITH GAS-TURBINE ENGINE ANTI-BLADDING SYSTEM
CN204757366U (en) Hot air stove
JPS57164240A (en) Air conditoner
CA2331168A1 (en) Flexible gas-fired heat exchanger system
RU2210679C2 (en) Air heating system for sets with gas turbine engine
RU2004136473A (en) METHOD FOR HEATING HEATING AND THERMAL FURNACES
SU1726801A1 (en) Device for secondary air supply
RU2002101385A (en) Combined cycle power plant with simultaneous combustion of solid and gaseous fuels
SU1746111A1 (en) Waste-heat boiler plant and method of its operation
RU2002120304A (en) Air-pressure device / barogenerator / and power plant with its use
RU2002117617A (en) The method of operation of the internal combustion engine and the regulator of heat exposure for its implementation
RU2002114394A (en) Gas turbine unit

Legal Events

Date Code Title Description
MM4A The patent is invalid due to non-payment of fees

Effective date: 20120601